发明名称 |
Gas turbine engine fan drive gear system damper |
摘要 |
A gas turbine engine includes a fan section. A turbine section is coupled to the fan section via a geared architecture. The geared architecture includes a torque frame and a flex support spaced apart from one another at a location. A gear train is supported by the torque frame. A damper is provided between the torque frame and the flex support at the location.
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申请公布号 |
US8573926(B2) |
申请公布日期 |
2013.11.05 |
申请号 |
US201213557515 |
申请日期 |
2012.07.25 |
申请人 |
COFFIN JAMES B.;OTTO JOHN R.;UNITED TECHNOLOGIES CORPORATION |
发明人 |
COFFIN JAMES B.;OTTO JOHN R. |
分类号 |
F01D25/04 |
主分类号 |
F01D25/04 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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